QUICK CONNECTION ASSEMBLIES ESPECIALLY USEFUL FOR COUPLING AIRCRAFT ANTENNA FAIRINGS TO AIRFRAME STRUCTURES
    21.
    发明公开
    QUICK CONNECTION ASSEMBLIES ESPECIALLY USEFUL FOR COUPLING AIRCRAFT ANTENNA FAIRINGS TO AIRFRAME STRUCTURES 审中-公开
    快速连接组件特别适用于连接飞机天线到飞机结构

    公开(公告)号:EP3239038A1

    公开(公告)日:2017-11-01

    申请号:EP17168703.1

    申请日:2017-04-28

    申请人: Embraer S.A.

    IPC分类号: B64C1/36 H01Q1/28 H01Q1/42

    摘要: Aircraft antenna fairing assemblies (20) include a fairing shell (30) and connection components (60, 70, 80, 90) for positionally fixing the fairing shell to airframe structure of an aircraft (10). The connection components comprise a guide assembly (60, 70) having a guide head (62b, 74b) and a receiver (64, 78) defining a guide channel for receiving the guide head therewithin, and a latch assembly (90) for latching the fairing shell to the airframe structure of the aircraft. The receiver of the guide assembly defines a generally C-shaped or generally U-shaped channel for receiving the guide head therewithin.

    摘要翻译: 飞行器天线整流罩组件(20)包括整流罩(30)和连接部件(60,70,80,90),用于将整流罩壳定位固定到飞机(10)的机身结构上。 连接部件包括具有导向头(62b,74b)和接收器(64,78)的导向组件(60,70),所述导向组件限定用于在其中接收导向头的导向通道,以及闩锁组件(90) 为飞机的机身结构罩壳。 引导组件的接收器限定用于在其中接收引导头的大致C形或大致U形的通道。

    Emergency gravity free-fall deployment systems for retractable aircraft landing gear assemblies
    23.
    发明公开
    Emergency gravity free-fall deployment systems for retractable aircraft landing gear assemblies 有权
    对于收放飞机起落架组件紧急重力自由下落部署系统

    公开(公告)号:EP2878534A1

    公开(公告)日:2015-06-03

    申请号:EP14195780.3

    申请日:2014-12-02

    申请人: Embraer, S.A.

    IPC分类号: B64C25/30

    摘要: Systems are disclosed to allow for the landing gear doors to be opened in the event of an emergency gravity free-fall landing gear deployment with little or no contact with the landing gear tires. The emergency gear extension systems according to the embodiments disclosed herein thus permit the free-fall movement of the landing gear to be synchronized with the opening of the associated gear doors. That is, according to the embodiments disclosed herein deployment of the landing gear assembly is time-delayed relative to the opening of the associated gear door(s). In such a manner, the landing gear assembly is synchronously released only after the associated gear door is in a safe position during its opening sequence thereby avoiding the risk that the gear door will jam the full extension of the landing gear during an emergency gear deployment due to contact between the landing gear tires and the gear door.

    Assemblies and methods for handling, transporting and/or positioning component parts
    24.
    发明公开
    Assemblies and methods for handling, transporting and/or positioning component parts 有权
    安排和处理,传输和/或组件的定位方法

    公开(公告)号:EP2799344A3

    公开(公告)日:2015-05-20

    申请号:EP14166891.3

    申请日:2014-05-02

    申请人: Embraer, S.A.

    IPC分类号: B64F5/00

    摘要: Assemblies and methods for the handling, transporting and/or positioning component parts include a jig assembly for supporting a component part is provided with an elongate spar assembly, a plurality of rib assemblies attached to the spar, and a plurality of tensionable strap assemblies operatively associated with the rib assemblies for capturing and holding the component part against the rib assemblies. The strap assemblies may include a strap ratchet mechanism and a strap, so that operation of the strap ratchet mechanism allows strap slack to be removed thereby tensioning the strap. The jig assembly may be positioned and oriented by suspension cables and a hoist mechanism to allow it to be removably connected to a moveable transport dolly.

    Passenger interface units and assemblies
    25.
    发明公开
    Passenger interface units and assemblies 审中-公开
    乘客接口单元和安排

    公开(公告)号:EP2803573A3

    公开(公告)日:2014-12-24

    申请号:EP14168595.8

    申请日:2014-05-16

    申请人: Embraer, S.A.

    IPC分类号: B64D11/00

    摘要: Passenger interface units include individual passenger modules (14a,14b) having co-located controls for passenger comfort and entertainment systems. The modules (14a,14b) will include a glass panel (40) having front and rear surfaces, a structural support panel (42) bonded to the rear surface of the glass panel (40) and a light-emitting unit (50) supported by the support panel (42) behind the rear surface of the glass panel (40). The rear surface of the glass panel (40) may include an opaque printed coating layer (46) having at least one unpainted region that is transparent to visible light emitted by the light-emitting unit (50) thereby allowing the visible light to be transmitted through the glass panel (40) and visible at the front surface thereof.

    Assemblies and methods for handling, transporting and/or positioning component parts
    26.
    发明公开
    Assemblies and methods for handling, transporting and/or positioning component parts 有权
    安排和处理,传输和/或组件的定位方法

    公开(公告)号:EP2799344A2

    公开(公告)日:2014-11-05

    申请号:EP14166891.3

    申请日:2014-05-02

    申请人: Embraer, S.A.

    IPC分类号: B64F5/00

    摘要: Assemblies and methods for the handling, transporting and/or positioning component parts include a jig assembly for supporting a component part is provided with an elongate spar assembly, a plurality of rib assemblies attached to the spar, and a plurality of tensionable strap assemblies operatively associated with the rib assemblies for capturing and holding the component part against the rib assemblies. The strap assemblies may include a strap ratchet mechanism and a strap, so that operation of the strap ratchet mechanism allows strap slack to be removed thereby tensioning the strap. The jig assembly may be positioned and oriented by suspension cables and a hoist mechanism to allow it to be removably connected to a moveable transport dolly.

    摘要翻译: 用于处理,传输和/或定位的部件组件和方法包括用于支持一个组成部分在细长节省装配,附接至翼梁肋组件被设置为多个用夹具组件,以及操作地相关联的张紧带组件一个多元化 与用于捕获和保持抵靠肋组件的组成部分的肋组件。 所述带组件可包括带棘轮机构和一个带所以没带棘轮机构的手术允许,由此以待除去带子松弛张紧带。 夹具组件可以被定位,并通过悬挂线缆导向和升降机构,以允许其可移除地连接到可移动运输台车。

    System and method for remote and automatic assessment of structural damage and repair
    29.
    发明公开
    System and method for remote and automatic assessment of structural damage and repair 审中-公开
    系统与Verfahren zur automatischen Fern-Bewertung von Strukturschaden und Reparatur

    公开(公告)号:EP2607239A2

    公开(公告)日:2013-06-26

    申请号:EP12199161.6

    申请日:2012-12-21

    申请人: Embraer , S.A.

    IPC分类号: B64F5/00 G06Q10/00 G07C5/00

    摘要: Structural analysis automation allows the implementation of more detailed or accurate analysis methodology that reflects the actual behavior of the damaged or repaired structure and consequently improves the resulting damage disposition for example by Increasing the allowable damages and structural repairs applicability, increasing the allowable damage limits causing the reduction of unnecessary installation of structural repairs, optimizing repairs and increasing fly-by periods and inspection intervals.

    摘要翻译: 结构分析自动化允许实施更详细或准确的分析方法,反映损坏或修理结构的实际行为,从而改善造成的损坏处置,例如增加允许的损坏和结构修复的适用性,增加允许的损伤限制, 减少不必要的结构维修安装,优化修理,逐步增加飞行时间和检查间隔。